Ip-based satellite command, control, and data transfer

Inactive Publication Date: 2016-11-24
MAHARAJA RISHABH Y
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0021]The system permits operations control on-orbit, in near real time within a secure system environment, with a dramatic increase in mission e

Problems solved by technology

However, TCP/IP does not perform well in networks having a large bandwidth-delay such as satellite links, and so it has not been very widely used by most of today satellite manufacturers.
Another problem with TCP/IP is its weakness to recover from frequent losses

Method used

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  • Ip-based satellite command, control, and data transfer
  • Ip-based satellite command, control, and data transfer
  • Ip-based satellite command, control, and data transfer

Examples

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Embodiment Construction

[0037]The present invention is a computerized system and method for IP-based satellite control in space, inclusive of the satellite bus architecture, ground control system architecture, and distributed software modules on both ends.

[0038]The following abbreviations are used throughout this application:

AOCS Attitude and Orbit Control Subsystem

C&DH Communication and Data Handling

CMD Command

COMM Communications

CPU Central Processing Unit

DSS Data Storage Subsystem

EPS Electric Power Distribution System

FTP File Transfer Protocol

HDD Hard Drive Device

HTTP Hypertext Transfer Protocol

IM Instant Messenger

IP Internet Protocol

MOC Mission Operations Center

[0039]USER / OPERATOR User at MOC

n.d. No Date

PCI Peripheral Component Interface

RAM Random Access Memory

RTG Radio Isotope Thermoelectric Generator

SCI Science

SD Secure Digital

SMTP Simple Mail Transfer Protocol

TCP Transmission Control Protocol

TDRS Tracking and Data Relay Satellite

TLM Telemetry

T&C Telemetry and Command

UDP User Datagram Protocol

USB Univ...

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PUM

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Abstract

A method and system for satellite control in space using an IP-based satellite bus and all-IP compliant subsystems and payload(s) and a corresponding T&C system. Specifically, the present method/system includes a satellite-based IP Bus (connected as a network) that relies on Ethernet, USB, WIFI, or Bluetooth to connect various satellite components, satellite components configured to communicate on the IP bus, and a T&C system that understands the IP bus and can read its telemetry and commands. The system permits operations control on-orbit, in near real time within a secure system environment, with a dramatic increase in mission efficiency, an expansion of how much and what can be done on-orbit, and cost savings on future missions using IP-compliant spacecraft and payloads.

Description

CROSS-REFERENCE TO RELATED APPLICATION(S)[0001]The present application derives priority from U.S. Provisional Patent Application 62 / 158,971 filed 8 May 2015.BACKGROUND OF THE INVENTION[0002]1. Field of the Invention[0003]The present invention relates to a method for satellite communications and, more particularly, to a satellite bus, its corresponding satellite subsystems, and a T&C that communicate by IP protocol.[0004]2. Description of the Background[0005]Satellites are proliferating for communication, surveillance, meteorology, navigation, etc. In each case a ground control system is needed for monitoring and controlling the satellite and its various payloads. The payloads are connected to a satellite bus, and commands are sent to the payloads via the satellite bus. For more information on the basics of satellite subsystems refer to Sellers et al., “Understanding Space: An Introduction to Astronautics”, McGraw-Hill Create (2005) ISBN 10: 0073407755).[0006]Telemetry and science da...

Claims

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Application Information

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IPC IPC(8): H04L29/12B64G1/24H04L29/08H04B1/38H04W4/00H04L12/40H04W4/80
CPCH04L61/2007H04W4/008H04L12/40B64G2001/245H04B1/38B64G1/242H04L67/02B64G1/428B64G1/66H04W4/80B64G1/244B64G1/245
Inventor MAHARAJA, RISHABH Y.
Owner MAHARAJA RISHABH Y
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